Formulation for flutter and vibration analysis of a hingeless helicopter blade in hover: Part I
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Emerald
Reference4 articles.
1. Rotary Wing Aeroelasticity-A Historical Perspective
2. Free vibration analysis of a rotating Timoshenko beam by differential transform method
3. Flapwise bending vibration analysis of a rotating tapered cantilever Bernoulli–Euler beam by differential transform method
4. Flapwise bending vibration analysis of double tapered rotating Euler–Bernoulli beam by using the differential transform method
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1. Nonlinear flexural response of a slender cantilever beam of constant thickness and linearly-varying width to a primary resonance excitation;Journal of Sound and Vibration;2017-02
2. Vibration Analysis of A Helicopter Blade with A Piezoelectric Actuated Trailing Edge Flap;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23
3. Rotorcraft research in India: recent developments;Aircraft Engineering and Aerospace Technology;2010-09-07
4. Vibration analysis of a rotating tapered Timoshenko beam using DTM;Meccanica;2009-05-28
5. Flexural–torsional-coupled vibration analysis of axially loaded closed-section composite Timoshenko beam by using DTM;Journal of Sound and Vibration;2007-10
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